FIELD OF THE INVENTION
[0001] This invention relates to the field of silicon carbide/graphite composite materials
and more particularly to dense, self-sintered silicon carbide/graphite composite materials.
BACKGROUND OF THE INVENTION
[0002] Silicon carbide is hard, strong, and exhibits good corrosion and abrasion resistance
and high thermal conductivity. It can be used in oxidizing temperatures up to 2500°F.
These properties render silicon carbide a useful material in many acid, caustic, corrosive,
abrasive, or high temperature environments. Such applications include pump seals and
bearings, gas turbine components, mixing nozzles, and flame holders.
[0003] Silicon carbide bodies are frequently formed by a sintering process. Sintered silicon
carbide has a high hardness, good corrosion resistance, and high thermal conductivity.
In sintering, particles of a material bond together when heated to a high temperature,
below the material's melting point. In some processes, the material is also subjected
to high pressure as well. A self-sintered process is one which does not require application
of pressure during the heating step for sintering to occur.
[0004] A drawback to silicon carbide is its lack of self-lubricity. A self-lubricating solid
is one having low friction in the absence of an additional lubricant. For example,
in applications having a high PV (pressure-sliding velocity) limit or dry running
applications, parts, such as seals, having a silicon carbide face adjoining a face
made of silicon carbide, other ceramics, or steel, will wear excessively due to the
forces generated by the high friction. In dry running applications with mating surfaces,
special wear surfaces must be provided on at least one of the bodies.
[0005] Graphite is a known lubricant and has been incorporated into carbon and silicon carbide
materials to impart a self-lubricating property to the material. However, with sintered
materials, it has been difficult to incorporate large amounts of a second phase such
as graphite into a ceramic matrix without causing cracks to occur in the microstructure
or without increasing the material's porosity. Further, adding graphite to silicon
carbide is even more difficult, because sintering of silicon carbide already requires
stringent conditions, such as fine, high purity powders, sintering aids, and high
temperature.
[0006] It is known to form a silicon carbide/graphite material by reaction bonding or reaction
sintering. However, reaction bonded silicon carbide/graphite material typically has
a residual silicon phase which limits corrosion resistance due to reaction with the
silicon in some chemical applications. Also, controlling the reaction bonding process
to obtain fully reacted and fully dense parts is difficult.
[0007] Another known silicon carbide material incorporating graphite is disclosed in U.S.
Patent No. 4,525,461. This material comprises a sintered silicon carbide/graphite/carbon
composite ceramic body having a homogeneous fine grain microstructure. At least 50%
of the silicon carbide grains are less than 8 µm, and the graphite grains have an
average size no larger than that of the silicon carbide grains. However, if the amount
of graphite is greater than approximately 8% by weight in this material, the material's
density decreases. Less than 8% by weight graphite, while providing a more dense,
impervious structure, limits the graphite's lubricating capability in the material.
[0008] Thus, there exists a need for a dense, impervious self-sintered silicon carbide body
with a greater amount of graphite inclusions to increase the lubricity of the material
while maintaining the integrity of the microstructure.
[0009] The present invention provides a process for producing a dense, self-sintered silicon
carbide/carbon graphite composite material comprising the steps of:
(a) providing a particulate mixture comprising:
(i) carbon-bonded graphite of between 2 and 30 percent by weight of the mixture, the
carbon-bonded graphite comprising at least 5 percent by weight carbon-precursor binder,
the balance being graphite,
(ii) between 1 and 10 percent by weight of a binder,
(iii) between 0.1 and 15 percent of a sintering aid,
(iv) between 1 and 5 percent by weight of a lubricant, and
(v) the balance being silicon carbide; and
(b) shaping the mixture to form a green body;
(c) heating the green body in a non-oxidising atmosphere at a carbonizing temperature
above 371°C (700°F) to carbonize the binder; and
(d) sintering the carbonized body at a temperature ranging from 1900°C to 2300°C in
a substantially inert atmosphere at or below atmospheric pressure to produce a sintered
body having a density of at least 80 percent of theoretical and a microstructure in
which the average grain size of the carbon-graphite is larger than the average grain
size of the silicon carbide.
[0010] The silicon carbide may comprise α-silicon carbide, β-silicon carbide, or a combination
of both
DESCRIPTION OF THE DRAWINGS
[0011] The invention will be more fully understood from the following detailed description
taken in conjunction with the accompanying drawings in which:
Fig. 1 is a schematic illustration of the process for producing a dense, self-sintered
silicon carbide/carbon-graphite composite material according to the present invention;
Fig. 2 is a table of test results;
Fig. 3 is an optical photomicrograph at 50X magnification of a silicon carbide/carbon-graphite
composite material according to the present invention;
Fig. 4 is a further optical photomicrograph at 50X magnification of a silicon carbide/carbon-graphite
composite material according to the present invention; and
Figs. 5a, 5b, 5c, and 5d are scanning electron micrographs at 50X, 500X, 1000X, and
2000X magnification respectively, of a further silicon carbide/carbon-graphite composite
material according to the present invention.
[0012] The process for producing the dense, self-sintered composite material of the present
invention is shown schematically in Fig. 1. The composite body is formed from a particulate
mixture of a silicon carbide matrix formulation and a carbon-bonded graphite. The
carbon binder for the graphite comprises a carbon-precursor resin capable of leaving
a carbon residue upon heating, to be described more fully below.
[0013] The silicon carbide matrix formulation may comprise a fine-grained, high purity α-silicon
carbide, β-silicon carbide, or a combination thereof. Preferably, at least 0.5 percent
α-silicon carbide relative to β-silicon carbide is present to achieve better densification.
A formulation comprising approximately 90 to 91 percent β-SiC, 4 to 5 percent a-SiC,
and 5 percent resin binder has been found to provide satisfactory results. The α-sic
and β-SiC may be supplied from any commercially available source.
[0014] Generally, a slurry of α-SiC and β-SiC in distilled water is prepared. The SiC is
typically provided in-powder form and should be fine-grained, having a BET surface
area of more than 5 m
2/g and preferably more than 10 m
2/g. Also, the powder should be of a high purity, generally at least 95 percent and
preferably 97 percent pure. Typically, a sintering aid, such as boron or boron carbide,
B
4C, is added to the SiC suspension. Other known sintering aids, such as aluminum or
beryllium or compounds thereof, may be provided if desired. Alternatively, a sintering
aid may be introduced at other known steps in the process of forming a sintered composite
body. A dispersant, for example, ammonium polymethacrylate, is generally added to
the slurry. The dispersant is a temporary additive not forming part of the final composite
body. The slurry is mixed, for example, in a ball mill for a period of time, typically
about eight hours, sufficient to disperse the ingredients. The slurry is then transferred
to a mixing tank.
[0015] The carbon-bonded graphite is prepared for addition to the SiC slurry. It comprises
at least 5 percent by weight of a carbon binder, the balance comprising a coarse graphite.
In the preferred embodiment, a mixture of approximately 70 to 80 percent graphite
and 20 to 30 percent binder is provided. A greater amount of binder may be used, although
the lubricating capability of the graphite in the final composite body may be reduced.
[0016] A coarse graphite such as Lonza KS-150, available from Lonza, Inc., Fairlawn, NJ,
in which 55 percent of the particles are larger than 45 µm, is suitable. A suitable
binder is a phenolic resin, although other materials which will decompose upon heating
to leave a carbon residue, such as furfuryl alcohol, polyester resin, coal tar pitch,
or mixtures of these and other materials, may be used. Upon decomposition, the binder
causes an increase in the porosity of the graphite particles, as discussed further
below.
[0017] The binder in powdered form is dissolved in acetone or any other suitable solvent
and mixed thoroughly with the graphite to bond the graphite particles. The mixture
is dried to evaporate the solvent and crushed to obtain carbon-bonded graphite particles
of the desired size. preferably, the carbon-bonded graphite is passed through a 200-mesh
sieve to obtain particles of less than 75 µm. The carbon-bonded graphite is then added
to the mixing tank with the SiC slurry. The carbon-bonded graphite generally comprises
between 2 and 30 percent by weight of the solids content of the mixture.
[0018] A resin solution in distilled water is also added to the mixing tank as a binder
for subsequent shaping of the particulate mixture to form a green body. The resin,
for example, phenolic resin, typically comprises 5 percent of the total SiC matrix
formulation. Also, a die lubricant, such as oleic acid, is generally added in an amount
equal to approximately 5 percent of the total SiC matrix formulation (SiC and resin
binder). The die lubricant, which is also a temporary additive not forming a part
of the final composite body, facilitates subsequent removal from the die in which
the particulate mixture is shaped.
[0019] The resulting slurry is mixed thoroughly and dried. Typically, the slurry is spray
dried to form spherical granules having an average size less than approximately 500
µm. Any other suitable methods for obtaining such granules may be used. For example,
the slurry may be pan dried, crushed to obtain a flour, and passed through a sieve
to obtain the desired particle size.
[0020] A measured amount of the particulate mixture is fed into a die and compacted, typically
at pressures ranging between 2 to 20 tons/in
2, to the desired shape to form a green body. Any other suitable method of shaping
the mixture may be employed. The shaped green body is carbonized in a non-oxidizing
atmosphere above 700°F. In a typical carbonization cycle, the component is heated
in an oven from room temperature to 350°F during a half hour period and allowed to
soak at that temperature for another half hour. The temperature is raised to 850°F
over a period of ten hours and held at 850°F for five hours to carbonize the resin.
The component is then cooled to room temperature. Other suitable carbonization cycles
may be used.
[0021] Next, the carbonized body is sintered at a temperature ranging from 1900°C to 2300°C,
preferably 2000°C to 2200°C, in a substantially inert atmosphere such as helium or
argon at or below atmospheric pressure. Generally, the temperature is raised to the
sintering temperature over an eight hour period, although the actual time depends
on the particular furnace used. The furnace is held at the peak temperature for one
hour and then allowed to cool to room temperature. Other suitable sintering cycles
may be used. Additionally, the carbonization cycle and the sintering cycle may be
carried out in separate furnaces or in a single furnace.
[0022] The process of the present invention results in a sintered composite body comprising
between 55 and 97.9 percent by weight silicon carbide, between 2 and 30 percent by
weight carbon-graphite, and between 0.1 and 15 percent by weight sintering aids. The
material has a density of at least 80 percent, and preferably 90 percent, of the theoretical
density of the particular mixture. This density may be achieved, since during carbonization,
part of the carbon-precursor binder for the graphite volatilizes, leaving voids, while
the remainder forms a coke residue on the graphite. Thus, the carbon-graphite particles
at this stage have a greater porosity than graphite alone. Subsequently during sintering,
the porous carbon-graphite collapses, allowing greater shrinkage of the SiC matrix
despite the presence of the carbon-graphite inclusions. Thus, a relatively dense and
impervious composite body results. The resulting composite body has a microstructure
in which the average grain size of the carbon-graphite is larger than the average
grain size of the silicon carbide. The average grain size of the carbon-graphite ranges
between 10 and 75 µm, and the average grain size of the silicon carbide ranges between
2 and 15 µm. Preferably, the carbon-graphite has an average grain size between 20
and 30 µm.
[0023] Tests of several different compositions were performed according to the present invention.
See Fig. 2. In test bake nos. 1-17, the silicon carbide matrix was provided by a mix
consisting of 90.25 percent of a fine-grained β-SiC powder having a BET surface area
of 13.5 to 18.5 m
2/g, 4.75 percent of a fine-grained α-SiC having a BET surface area of 9.0 to 11.0
m
2/g, and 5.0 percent liquid phenolic resin. In test bake no. 18, the silicon carbide
matrix was provided by 100 percent α-SiC having a BET surface area of 15 m
2/g. B
4C was used as a sintering aid, comprising approximately one percent of the total mix.
Oleic acid was added as a die lubricant in an amount comprising approximately 5.0
percent of the total mix. These components are readily available from known commercial
sources.
[0024] Several grades of graphite were tested to determine which provided the best sinterability:
a fine graphite in which 50 percent of the particles are smaller than 2.4 µm, a coarse
graphite in which 55 percent of the particles are larger than 45 µm, and a coarse,
resin-bonded graphite in which 50 percent of the particles are larger than 74 µm.
The fine graphite used in the tests was Lonza KS-6, commercially available from Lonza,
Inc. The coarse graphite used was Lonza KS-150, also commercially available from Lonza,
Inc. The coarse, carbon-bonded graphite was specially mixed as described above and
consisted of 20 percent by weight phenolic resin and 80 percent by weight Lonza KS-150.
[0025] In the tests, the composite body was formed by mixing a slurry of the silicon carbide
with the graphite or carbon-bonded graphite. The mixture was dried and granulated
and molded at 2 to 20 tons per square inch. The molded green body was carbonized at
850°F, and the carbonized body was sintered at temperatures of 2070°C and 2090°C.
[0026] Test results are shown in Fig. 2. In some test bakes, the graphite was sieved prior
to mixing with the silicon carbide to obtain a specific size range. This is indicated
in the column "Graphite Size." The entry "Unsized" indicates that the graphite was
not sieved. The sieved graphite is indicated by the appropriate size ranges. The specially
mixed carbon-bonded graphite is designated Mix No. 1 in the column labeled "Graphite
Type."
[0027] The tests show that samples containing large amounts of the commercially available
non-carbon-bonded graphites, i.e., the fine graphite, Lonza KS6, and the coarse graphite,
Lonza KS150, (Test Bake Nos. 3-8) did not provide satisfactory results. The resulting
sintered samples were too porous, as indicated by the percent of water absorption,
and did not achieve sufficient densification.
[0028] The samples using the specially mixed coarse, carbon-bonded graphite (Test Bake Nos.
9-17) indicate that greater densification was achieved with a graphite loading of
15 percent by weight than has been achieved in prior art composite bodies using a
comparable loading of non-carbon-bonded graphite. Some lamination in removal from
the die, leading to some water absorption, occurred using the larger graphite particles.
Lamination did not occur when carbon-bonded graphite particles small enough to pass
through the 200-mesh sieve, that is, less than 75 µm, were used.
[0029] Silicon carbide/carbon-graphite composite materials according to the present invention
are shown in the photomicrographs of Figs. 3 through 5. The carbon-graphite appears
as the darker inclusions among the lighter silicon carbide matrix. Fig. 3 shows an
optical micrograph of a polished cross-section of test bake no. 11 magnified 50 times
(50X). The material appears fully dense and the carbon-graphite is uniformly distributed.
[0030] Fig. 4 shows an optical micrograph of a polished cross-section of test bake no. 17
at 50X magnification. The material appears fully dense and the carbon-graphite is
uniformly distributed.
[0031] Figs. 5a through 5d show scanning electron micrographs at 50X, 500X, 1000X, and 2000x
magnification respectively of test bake no. 17 polished and etched to show the grain
structure. The grain size of the silicon carbide is less than 10 µm, and the carbon-graphite
grain size is in the range of 20 to 60 µm.
[0032] The invention is not to be limited by what has been particularly shown and described,
except as indicated in the appended claims.
1. A process for producing a dense, self-sintered silicon carbide/carbon graphite composite
material comprising the steps of:
(a) providing a particulate mixture comprising:
(i) carbon-bonded graphite of between 2 and 30 percent by weight of the mixture, the
carbon-bonded graphite comprising at least 5 percent by weight carbon-precursor binder,
the balance being graphite,
(ii) between 1 and 10 percent by weight of a binder,
(iii) between 0.1 and 15 percent of a sintering aid,
(iv) between 1 and 5 percent by weight of a lubricant, and
(v) the balance being silicon carbide; and
(b) shaping the mixture to form a green body;
(c) heating the green body in a non-oxidising atmosphere at a carbonizing temperature
above 371°C (700°F) to carbonize the binder; and
(d) sintering the carbonized body at a temperature ranging from 1900°C to 2300°C in
a substantially inert atmosphere at or below atmospheric pressure to produce a sintered
body having a density of at least 80 percent of theoretical and a microstructure in
which the average grain size of the carbon-graphite is larger than the average grain
size of the silicon carbide.
2. The process of claim 1, wherein the carbon-precursor binder comprises phenolic resin,
furfuryl alcohol resin, polyester resin, coal tar pitch, or mixtures thereof.
3. The process of claim 1 or claim 2, wherein the carbonized body is sintered at a temperature
ranging from 2100°C to 2200°C.
4. The process of any preceding claim, wherein the carbon-bonded graphite has a particle
size less than about 75 µm.
5. The process of any preceding claim, wherein the silicon carbide comprises at least
0.5 percent by weight α-silicon carbide, the balance being β-silicon carbide.
6. The process of any preceding claim, wherein the carbon-bonded graphite comprises between
20 and 30 percent by weight carbon-precursor resin and between 70 and 80 percent by
weight graphite.
7. The process of any preceding claim, wherein the silicon carbide comprises approximately
95 percent by weight β-silicon carbide and approximately 5 percent by weight α-silicon
carbide.
8. The process of any preceding claim, wherein the silicon carbide has a BET surface
area less than 50 m2/g.
9. The process of any preceding claim, wherein the silicon carbide has a BET surface
area less than 20 m2/g.
10. The process of any preceding claim, wherein the carbon-bonded graphite is prepared
by providing a mixture of a coarse graphite and a carbon-precursor binder dissolved
in a solvent, drying the mixture and crushing to obtain particles of less than 75
µm.